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355.0 Aluminum vs. ASTM A369 Grade FP92

355.0 aluminum belongs to the aluminum alloys classification, while ASTM A369 grade FP92 belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 355.0 aluminum and the bottom bar is ASTM A369 grade FP92.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 72 to 83
210
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 1.5 to 2.6
19
Fatigue Strength, MPa 55 to 70
330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 150 to 240
440
Tensile Strength: Ultimate (UTS), MPa 200 to 260
710
Tensile Strength: Yield (Proof), MPa 150 to 190
490

Thermal Properties

Latent Heat of Fusion, J/g 470
260
Maximum Temperature: Mechanical, °C 180
590
Melting Completion (Liquidus), °C 620
1490
Melting Onset (Solidus), °C 560
1450
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 150 to 170
26
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38 to 43
9.3
Electrical Conductivity: Equal Weight (Specific), % IACS 120 to 140
10

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.0
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1120
89

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.7 to 5.9
120
Resilience: Unit (Modulus of Resilience), kJ/m3 150 to 250
620
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 20 to 27
25
Strength to Weight: Bending, points 28 to 33
22
Thermal Diffusivity, mm2/s 60 to 69
6.9
Thermal Shock Resistance, points 9.1 to 12
19

Alloy Composition

Aluminum (Al), % 90.3 to 94.1
0 to 0.020
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0 to 0.25
8.5 to 9.5
Copper (Cu), % 1.0 to 1.5
0
Iron (Fe), % 0 to 0.6
85.8 to 89.1
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.5
0.3 to 0.6
Molybdenum (Mo), % 0
0.3 to 0.6
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.040 to 0.090
Nitrogen (N), % 0
0.030 to 0.070
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 4.5 to 5.5
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.25
0 to 0.010
Tungsten (W), % 0
1.5 to 2.0
Vanadium (V), % 0
0.15 to 0.25
Zinc (Zn), % 0 to 0.35
0
Zirconium (Zr), % 0
0 to 0.010
Residuals, % 0 to 0.15
0